1. Calculate the centroid, moment of inertia about the horizontal axis XX (Neutral Axis), Section modulus,...

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1. Calculate the centroid, moment of inertia about the horizontal axis XX (Neutral Axis), Section modulus, and Radius of Gyration of the I-beam section used as a spar in the wing structure of an aircraft. All dimensions are in mm. 250.00 38.00 25.00 I 300.00 A- 38.00 150.00 1. Calculate the centroid, moment of inertia about the horizontal axis XX (Neutral Axis), Section modulus, and Radius of Gyration of the I-beam section used as a spar in the wing structure of an aircraft. All dimensions are in mm. 250.00 38.00 25.00 I 300.00 A- 38.00 150.00